JPS609589Y2 - gas stove - Google Patents
gas stoveInfo
- Publication number
- JPS609589Y2 JPS609589Y2 JP14412680U JP14412680U JPS609589Y2 JP S609589 Y2 JPS609589 Y2 JP S609589Y2 JP 14412680 U JP14412680 U JP 14412680U JP 14412680 U JP14412680 U JP 14412680U JP S609589 Y2 JPS609589 Y2 JP S609589Y2
- Authority
- JP
- Japan
- Prior art keywords
- combustion
- pilot burner
- flame
- combustion tube
- gas stove
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Landscapes
- Gas Burners (AREA)
Description
【考案の詳細な説明】
本考案は、パイロットバーナによりメインバーナに着火
させる構成のガスストーブに関するもので、特にパイロ
ットバーナ着火部のまわりに、側壁を設けて、火炎のひ
ろがりを抑制しようとするものである。[Detailed Description of the Invention] The present invention relates to a gas stove configured to ignite a main burner with a pilot burner. In particular, a side wall is provided around the pilot burner ignition part to suppress the spread of the flame. It is.
従来、ガイドを有さない点火装置にあっては、パイロッ
ト火炎は、パイロットバーナより噴出後空気と拡散して
ひろがり、また拡散燃焼式ストーブにおいて、パイロッ
トバーナ6の火炎が外燃焼筒予混合部に衝突する場合は
、衝突後外燃焼筒に沿って円周方向へひろがる。Conventionally, in an ignition device without a guide, the pilot flame ejects from the pilot burner and then spreads out with the air, and in a diffusion combustion stove, the flame of the pilot burner 6 flows into the premixing section of the outer combustion tube. In the case of a collision, it spreads in the circumferential direction along the outer combustion tube after the collision.
その結果、パイロットバーナの火炎は外燃焼筒燃焼部に
接触する範囲がひろくなり、メインバーナの2次空気と
の拡散を妨げる結果メインガスの吹き飛びをおこしたり
パイロット点火時の火災の伸びが高くなる欠点があった
。As a result, the area in which the pilot burner flame comes into contact with the combustion part of the outer combustion tube becomes wider, which prevents the flame from diffusing with the secondary air of the main burner, causing the main gas to blow away and increasing the spread of the fire during pilot ignition. There were drawbacks.
また、パイロットバーナの流量を小さくした場合には、
パイロット火炎が円周方向にひろがるため、外燃焼筒燃
焼部まで到達できず、メインガスへ着火用の火炎を供給
できなくなり、着火性能が悪くなる欠点もあった。Also, if the flow rate of the pilot burner is reduced,
Since the pilot flame spreads in the circumferential direction, it cannot reach the combustion section of the outer combustion tube, making it impossible to supply ignition flame to the main gas, resulting in poor ignition performance.
本考案は上記従来技術の問題点を改良するものである。The present invention improves the problems of the prior art described above.
以下本考案の詳細について、図面とともに説明する。The details of the present invention will be explained below with reference to the drawings.
第1図から第3図は本考案の一実施例を示すものであり
、図において1は主バーナ燃料噴出部、2は外燃焼筒予
混合部、3は外燃焼筒燃焼部、4は内燃鏡筒予混合部、
5は内燃鏡筒燃焼部、6は点火用パイロットバーナ、7
はコック、8はガラス筒、9はドラフタ、10はガラス
受は台、11は圧電点火プラグ、12はガイドである。1 to 3 show an embodiment of the present invention, and in the figures, 1 is the main burner fuel injection part, 2 is the external combustion tube premixing part, 3 is the external combustion cylinder combustion part, and 4 is the internal combustion cylinder. lens barrel premixing section,
5 is an internal combustion barrel combustion section, 6 is a pilot burner for ignition, and 7 is an ignition pilot burner.
8 is a cock, 8 is a glass cylinder, 9 is a drafter, 10 is a glass receiver stand, 11 is a piezoelectric spark plug, and 12 is a guide.
まず第1図によって拡散燃焼型ガスストーブの構成と燃
焼方式について述べる。First, the configuration and combustion method of a diffusion combustion type gas stove will be described with reference to Figure 1.
コック7開後燃料ガスはメインバーナ1、及び点火用パ
イロットバーナ6より同時に噴出する。After the cock 7 is opened, fuel gas is simultaneously ejected from the main burner 1 and the ignition pilot burner 6.
メインバーナ1より噴出したガスは内外燃焼筒燃焼部3
,5に至る内外燃焼筒間の通路において内外燃焼筒予混
合部2に設けられた多数の孔より流入する空気と混合し
ながら燃焼部3に至る。The gas ejected from the main burner 1 is transferred to the combustion section 3 of the inner and outer combustion tubes.
.
一方点火用パイロットバーナ6の炎は外燃鏡筒予混合部
2を加熱し一部外燃鏡筒子混合部2の孔より未燃及び既
燃のガスを内外燃焼筒間に供給しながら、外燃鏡筒2に
沿って上昇して燃焼部3まで到達しメインバーナのガス
に着火する。On the other hand, the flame of the pilot burner 6 for ignition heats the external combustion tube premixing section 2 and partially supplies unburned and burnt gas from the hole in the external combustion tube mixing section 2 between the inner and outer combustion tubes. It ascends along the combustion barrel 2 and reaches the combustion section 3, where it ignites the gas in the main burner.
着火後予混合ガスの一部は内燃焼筒燃焼部5の孔より流
入する2次空気と反応しながら内外燃焼筒間に炎を形威
し、一部は外燃焼筒燃焼部3の炎孔より外へでて、外燃
焼筒とガラス筒8及びドラフタ9とによるドラフト効果
によって外燃燃焼筒2とガラス受は台10との間隙より
流入してくる2次空気と反応しながら外燃鏡筒燃焼部3
外側に火炎を形成する。After ignition, a part of the premixed gas reacts with the secondary air flowing in from the holes in the combustion part 5 of the inner combustion cylinder, forming a flame between the inner and outer combustion cylinders, and a part of the premixed gas forms a flame between the combustion parts 3 of the outer combustion cylinder. The external combustion cylinder 2 and the glass receiver react with the secondary air flowing in from the gap with the stand 10 due to the draft effect of the external combustion cylinder, the glass cylinder 8, and the drafter 9. Cylindrical combustion section 3
Forms a flame on the outside.
次に本考案の作用について詳しく説明する。Next, the operation of the present invention will be explained in detail.
第3図において、起動時において、パイロットバーナ火
炎は、外燃焼筒予混合部2に衝突するがガイド側壁端面
と外燃焼筒予混合部との間隙は消炎距離以下であるため
パイロットバーナ火炎は側方へ拡がらず、ガイドと外燃
焼筒予混合部2に沿って上昇し、ガイド上面の間隙を通
過して燃焼部3に至りメインガスに着火する。In Fig. 3, at startup, the pilot burner flame collides with the outer combustion tube premixing section 2, but since the gap between the guide side wall end face and the outer combustion tube premixing section is less than the extinguishing distance, the pilot burner flame collides with the outer combustion tube premixing section 2. It does not spread toward the direction, but rises along the guide and the outer combustion tube premixing section 2, passes through the gap between the upper surfaces of the guide, reaches the combustion section 3, and ignites the main gas.
このとき、パイロットバーナ火炎の幅が制限されて狭い
ため、パイロットバーナ流量が少ない場合でも、燃焼部
3まで火炎が到達できる利点がある。At this time, since the width of the pilot burner flame is limited and narrow, there is an advantage that the flame can reach the combustion section 3 even when the pilot burner flow rate is small.
また、燃焼部3を接触して流れるパイロット火炎の幅が
狭いため、メインガスと干渉する範囲が狭くなり、パイ
ロット点火時の火炎の伸びがすくなくなる。Furthermore, since the width of the pilot flame flowing in contact with the combustion section 3 is narrow, the range of interference with the main gas is narrowed, and the flame elongation during pilot ignition is reduced.
なお、ガイド12の上部に天板を設けて閉ざした方がパ
イロットバーナの広がりが小さくてよいが、外燃焼筒と
天板端面との間隙は消炎距離以下にせねばパイロットバ
ーナの着火性能が悪くなる。It should be noted that if the guide 12 is closed by providing a top plate, the spread of the pilot burner will be smaller, but the ignition performance of the pilot burner will deteriorate unless the gap between the outer combustion tube and the end face of the top plate is less than the extinguishing distance. .
以上のような本考案は、パイロットの火炎のひろがりを
制限するガイドを設けるこにより、パイロット流量の少
ない場合でも着火性能がすぐれパイロット点火時の火炎
の伸びが少なくなるものである。The present invention as described above provides excellent ignition performance even when the pilot flow rate is low and reduces the flame extension during pilot ignition by providing a guide that limits the spread of the pilot flame.
また、ガイドを外燃焼筒とは分離して設けることができ
、組立精度の許容範囲が広く、組立が容易である。Furthermore, the guide can be provided separately from the outer combustion tube, allowing for a wide range of assembly accuracy and ease of assembly.
第1図は本考案の一実施例のガスストーブの断面図、第
2図は第1図のA−A線断面図、第3図は点火用パイロ
ットバーナ、燃焼筒及びガイドの構成を示した一部破断
斜視図である。
1・・・・・・燃料噴出部、2・・曲外燃焼筒予混合部
、3・・・・・・外燃焼筒燃焼部、4・曲・内燃焼筒予
混合部、5・・・・・・内燃焼筒燃焼部、6・曲・点火
用パイロットバーナ、7・・・・・・コック、訃・・・
・・ガラス筒、9・・・・・・ドラフタ、10・・・・
・・ガラス受は台、11・・・・・・圧電点火プラグ、
12・・・・・・ガイド。Fig. 1 is a sectional view of a gas stove according to an embodiment of the present invention, Fig. 2 is a sectional view taken along the line A-A in Fig. 1, and Fig. 3 shows the configuration of the ignition pilot burner, combustion tube, and guide. It is a partially cutaway perspective view. DESCRIPTION OF SYMBOLS 1... Fuel injection part, 2... Outer combustion tube premixing part, 3... Outer combustion tube combustion part, 4... Curved/inner combustion tube premixing part, 5... ...Inner combustion cylinder combustion section, 6. Pilot burner for bending and ignition, 7..Cook, tail...
...Glass tube, 9...Drafter, 10...
...Glass holder is stand, 11...Piezoelectric spark plug,
12...Guide.
Claims (2)
スストーブにおいて、前記外燃鏡筒外にパイロットバー
ナ噴出部を配し、前記外燃鏡筒にパイロットバーナ導入
孔を形威し、前記外燃鏡筒とガイドで前記パイロットバ
ーナ噴出部をかこんだガスストーブ。(1) In a gas stove that ejects and burns gas between an internal combustion tube and an external combustion tube, a pilot burner ejection part is disposed outside the external combustion tube, and a pilot burner introduction hole is formed in the external combustion tube. A gas stove in which the pilot burner ejection part is surrounded by the external combustion barrel and the guide.
ある実用新案登録請求の範囲第1項記載のガスストーブ
。(2) The gas stove according to claim 1, wherein the gap between the guide end face and the external combustion barrel is equal to or less than the flame extinction distance.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14412680U JPS609589Y2 (en) | 1980-10-09 | 1980-10-09 | gas stove |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14412680U JPS609589Y2 (en) | 1980-10-09 | 1980-10-09 | gas stove |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5766374U JPS5766374U (en) | 1982-04-20 |
JPS609589Y2 true JPS609589Y2 (en) | 1985-04-04 |
Family
ID=29503845
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14412680U Expired JPS609589Y2 (en) | 1980-10-09 | 1980-10-09 | gas stove |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS609589Y2 (en) |
-
1980
- 1980-10-09 JP JP14412680U patent/JPS609589Y2/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS5766374U (en) | 1982-04-20 |
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